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APP Zºſº IX 2 MUMEPICAL FUNCTIONAPPROXIMATIONS 35
COMPUTER PROGRAM FøRTRAN CODES 39
INPUT AND OUTPUT FOR SAMPLE CASES
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analysis angle of attack angle of sideslip application assigned boattail boundary buckling calculated CARD Center characteristics chondrite Classification Map clusters coefficient comparison Continued corner correction crack curve data set deflection determined diffuser drag DUCT effects equation error estimated factor Figure flap flow Forest function geometry given ground truth included indicate INPUT length Linear loading loss Mach number maximum measured method NASA NSECT obtained output parameters percent performance pixel plotted points position presented pressure range ratio RECT reference region Report Reynolds number samples shape shock shown shows similarity Space specimens spoiler stress surface Table techniques test section turning V/STOL vane variation wind tunnel wing